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The Enstrom F-28F is equipped with a Lycoming HIO-360-F1AD engine. HIO-360-A1A 180 hp (134 kW) at 2900 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the IO-360-A1A except that it has a Bendix RSA-5AB1 fuel injector, Bendix S4LN-200 magnetos and lacks provision for propeller governor drive. [4] HIO-360-A1B
The first O-360 certified was the A1A model, certified on 20 July 1955 to United States CAR 13 effective March 5, 1952 as amended by 13-1 and 13-2. [4] The Lycoming IO-390 is an O-360 which has had its cylinder bore increased by 3 ⁄ 16 inch (4.8 mm), developing 210 hp (160 kW).
The prototype SIAI S.205 exhibited at the Paris Air Show in June 1965 S.205 basic version, metal, single-engine four-seat airplane, the F version had a fixed undercarriage, while the R version had a retractable undercarriage. It was offered with three different engines: S.205 F/R-18: Avco Lycoming O-360 S.205 F/R-20: Avco Lycoming IO-360-A1A
Same as IO-360-A except for reduced compression ratio and rated power. The crankshaft has two 6th order dampers. [4] IO-360-C 210 hp (157 kW) at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for accessory drive provisions. The crankshaft has two 6th order ...
One, sold by the current owner of the Sedan design, replaces many of the components ahead of the firewall with updated versions, including a Lycoming O-360-A1A engine of 180 horsepower (130 kW), a constant speed propeller, a new engine mount, and a fiberglass cowling. A second modification from the design holder allows the removal of the oil ...
The current engine is a Lycoming IO-360-A1B6, giving the Fury a max speed of 222 mph. The aircraft will carry two adults with up to 100 pounds of baggage and has a range of 1000 miles. The aircraft will carry two adults with up to 100 pounds of baggage and has a range of 1000 miles.
Jack Riley, the designer of that aircraft was interested in an upgraded version of the Lycoming O-320 that would produce more power to give the Twin Navion a better single-engine service ceiling. The Lycoming O-360 was still years away in development and so a modification of the O-320 was undertaken by Lycoming. The O-320 received longer ...
The first production aircraft, powered by a 180 hp (134 kW) Lycoming O-360-A1A engine, first flew on October 21, 1957. In 1958, it was joined by a higher-powered PA-24-250 with a 250 hp (186 kW) Lycoming O-540-A1A5 engine; this model was originally to be known as the PA-26, but Piper decided to keep the PA-24 designation.